SDR ASOA1224

Service difficulty report · Drag Angle · Cndair CL6002C10

Difficulty date
September 26, 2008
Submitted
October 20, 2008
Operation
Air carrier
Make and model
Cndair CL6002C10
Part
Drag Angle
Condition
Cracked
Location
Vertical Stab
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

PERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, LEFT SIDE. FORWARD AND AFT DRAG ANGLES VERIFIED CRACKED, FORWARD DRAG ANGLE IS MARKED AT END OF CRACK. REPAIR OF AFT DRAG ANGLE. REMOVED DAMAGED AREA FROM FWD DRAG ANGLE ANGLE AND CLEANED UP CUT LINES TAKING CARE NOT TO DAMAGE UNDERLYING STRUCTURE PER NOTE 1 AND 2 OF REO 670-55-31-018. FABRICATED REPAIR FILLERS AND DOUBLERS USING 2024 T3 .090. PERFORMED LPI, NO DEFECTS NOTED. APPLIED PRIMER TO REPAIR FILLER AND DOUBLER AND CUT LINE PER NOTE 5 AND 6 OF REO 670-55-31-018. INSTALLED FASTENERS IN FILLER AND DOUBLER TO REPAIR AREA. FAY SEALED AND APPLIED A023 FINISH TO REPAIR AREA PER STEP 9 OF REO 670-55-31-018 JOB COMPLETED AS REQUIRED. SUPPLEMENTAL SDR CLOSED 10/20/08.